Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:cancellationDate |
technical and budgetary issues
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
9.2 meters
|
| gptkbp:engineType |
linear aerospike engine
|
| https://www.w3.org/2000/01/rdf-schema#label |
VentureStar
|
| gptkbp:intendedOperator |
gptkb:NASA
|
| gptkbp:intendedUse |
reusable launch vehicle
|
| gptkbp:launchSite |
gptkb:Kennedy_Space_Center_(planned)
|
| gptkbp:length |
38 meters
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:material |
composite materials
|
| gptkbp:notableFeature |
lifting body design
single-stage-to-orbit design intended to replace Space Shuttle no external boosters |
| gptkbp:payloadToLEO |
20,000 kg
|
| gptkbp:predecessor |
gptkb:X-33
|
| gptkbp:projectEndDate |
2001
|
| gptkbp:propulsion |
hydrogen-oxygen rocket
|
| gptkbp:reusable |
fully reusable
|
| gptkbp:seatingCapacity |
4
|
| gptkbp:startYear |
1996
|
| gptkbp:status |
cancelled
|
| gptkbp:successor |
none
|
| gptkbp:bfsParent |
gptkb:X-33
|
| gptkbp:bfsLayer |
5
|